View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 54766U 26145.49198248 +.00000000 +00000-0 +69739-4 0 00002
2 54766 53.2139 59.3345 0001075 98.8213 261.2901 15.08835510 03
| Epoch (UTC): | 25 May 2026 11:48:27 |
| Eccentricity: | 0.0001075 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.3345° |
| argument of perigee: | 98.8213° |
| revolutions per day: | 15.08835510 |
| mean anomaly at epoch: | 261.2901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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